Low-altitude logistics monitoring device based on temperature and humidity sensor

By designing buffer springs, support frames, and drawer structures on multi-rotor drones, the vibration problem during drone landing was solved, the temperature and humidity sensors were protected, and real-time temperature and humidity monitoring and cargo protection for low-altitude logistics were achieved.

CN223618913UActive Publication Date: 2025-12-02RES INST OF HIGHWAY MINIST OF TRANSPORT
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Patent Information

Application Number
CN202520093948.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-01-15
Publication Date
2025-12-02
Estimated Expiration
2035-01-15

AI Technical Summary

Technical Problem

Existing multi-rotor drone transport systems generate vibrations during landing, which damage sensors inside refrigerated containers, leading to equipment failure.

Method used

A low-altitude logistics monitoring device based on temperature and humidity sensors was designed, including a buffer spring, a support frame, a plastic disc, and a drawer structure. The buffer spring absorbs vibrations, the plastic disc prevents impacts, and the drawer separates goods to protect the temperature and humidity sensors from damage.

Benefits of technology

It effectively reduces the damage of vibration to temperature and humidity sensors, improves the service life of sensors, and monitors the temperature and humidity of goods in real time to prevent spoilage or melting of goods.

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Abstract

The low-altitude logistics monitoring device based on the temperature and humidity sensor comprises a multi-rotor unmanned aerial vehicle, a receiving assembly is fixedly installed in the center of the bottom end of the multi-rotor unmanned aerial vehicle, supporting legs are symmetrically and fixedly installed at the bottom end of the multi-rotor unmanned aerial vehicle, and the supporting legs are located on the two sides of the receiving assembly. The receiving assembly comprises a temperature control part and a collecting device, the temperature control part is fixedly installed in the center of the bottom end of the collecting device, the temperature control part comprises a protection device and a connecting device, and the protection device is fixedly installed in the center of the interior of the connecting device; the protection device comprises positioning rods, a pressing cross rod, a temperature and humidity sensor, bolts, a plastic circular plate, a supporting frame and supporting bottom plates, the positioning rods are fixedly installed at the four corners of the bottom end of the temperature and humidity sensor, and the supporting bottom plates are fixedly installed at the four corners of the interior of the supporting frame. According to the utility model, through the arrangement of the receiving assembly, the purpose of preventing the temperature and humidity sensor from being damaged by vibration is achieved.
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Description

Technical Field

[0001] This utility model relates to the field of transportation technology, specifically a low-altitude logistics monitoring device based on temperature and humidity sensors. Background Technology

[0002] Low-altitude logistics refers to a new logistics method that utilizes aircraft such as drones for delivery within low-altitude airspace. As an emerging, efficient, and modern transportation mode, low-altitude logistics has been piloted in areas such as express delivery, agricultural product transportation, and medical supply delivery, and is gradually changing the traditional transportation and logistics operation model. Multi-rotor drones have advantages such as vertical take-off and landing, hovering, and ease of operation, making them suitable for short- and medium-distance low-altitude logistics, and they have significant advantages and development potential in low-altitude cold chain logistics distribution.

[0003] For example, a logistics multi-rotor drone and logistics transportation system is disclosed in Chinese Patent Publication No. CN209553514U. This logistics multi-rotor drone includes a fuselage and a cargo bay; the cargo bay is connected to the fuselage and is used to transport goods. The cargo bay is made of a flexible material or an elastic material.

[0004] The multi-rotor drone transport system in the aforementioned patent can only achieve the purpose of securing and fixing goods. However, existing multi-rotor drone transport systems generate vibrations during landing, which can damage the sensors inside the refrigerated and insulated box over time. Therefore, an improved device is needed to address this issue. Utility Model Content

[0005] The purpose of this invention is to provide a low-altitude logistics monitoring device based on a temperature and humidity sensor to solve the problems mentioned in the background art.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a low-altitude logistics monitoring device based on a temperature and humidity sensor, comprising a multi-rotor drone, wherein a receiving component is fixedly installed at the center of the bottom end of the multi-rotor drone, and support feet are symmetrically fixedly installed at the bottom end of the multi-rotor drone, with the support feet located on both sides of the receiving component. The receiving component includes a temperature control component and a collection device. The temperature control component is fixedly installed at the center of the bottom end of the collection device. The temperature control component includes a protective device and a connecting device. The protective device is fixedly installed at the center of the interior of the connecting device.

[0007] Preferably, the protective device includes a positioning rod, a pressing crossbar, a temperature and humidity sensor, bolts, a plastic round plate, a support frame, and a support base plate. The positioning rod is fixedly installed at the four bottom corners of the temperature and humidity sensor, the support base plate is fixedly installed at the four inner corners of the support frame, the plastic round plate is fixedly installed at the four outer corners of the support frame, the bolts are symmetrically rotated and installed at the top of the support frame, and the pressing crossbar is threaded onto the outer ring of the bolts.

[0008] Preferably, the connecting device includes a buffer spring and a supporting cavity. The buffer spring is symmetrically fixedly installed at the top inside of the supporting cavity. The connecting device includes a buffer spring, a supporting cavity, a plastic strip, a U-shaped positioning frame, and an electric push rod. The buffer spring is symmetrically fixedly installed at the top inside of the supporting cavity. The electric push rod is symmetrically fixedly installed at the bottom inside of the supporting cavity. The U-shaped positioning frame is fixedly installed on the end of the electric push rod near the buffer spring. The plastic strip is fixedly installed on the side end of the U-shaped positioning frame away from the electric push rod. The collecting device includes an insulated cargo compartment, a drawer, and a guide rail. The guide rail is symmetrically fixedly installed on both sides inside the insulated cargo compartment. The drawer is slidably inserted into the guide rail.

[0009] Preferably, the support frame is fixedly installed on the end of the buffer spring away from the support cavity, the support cavity is fixedly installed at the bottom center of the insulated cargo box, and the insulated cargo box is fixedly installed at the bottom center of the multi-rotor UAV.

[0010] Preferably, the positioning rod is slidably inserted into the top of the support base plate.

[0011] Preferably, the drawer is fixedly equipped with keypads on both sides, and the guide rail is provided with a slot near the inside of the drawer. The temperature and humidity sensor is wirelessly connected to the ground signal receiving device, and the multi-rotor UAV is equipped with a temperature and humidity alarm module.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0013] When in use, this device is connected to the support frame via a buffer spring, which reduces the transmission of vibration. At the same time, bolts can move the pressing crossbar downwards, which can compress and secure the temperature and humidity sensor to the support base plate, thereby fixing the temperature and humidity sensor in place. Furthermore, the plastic circular plate prevents the support frame from colliding with the support cavity. Additionally, the drawer design can separate objects, preventing excessive accumulation of items inside the insulated cargo compartment, thus completing the vibration protection function for the temperature and humidity sensor. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the main structure of this utility model;

[0015] Figure 2 This is a schematic diagram of the receiving component structure of this utility model;

[0016] Figure 3 This is a schematic diagram of the temperature control component of this utility model;

[0017] Figure 4 This is a schematic diagram of the protective device structure of this utility model;

[0018] Figure 5 This is a schematic diagram of the connecting device structure of this utility model;

[0019] Figure 6 This is a schematic diagram of the collection device structure of this utility model;

[0020] Figure 7 This is a schematic diagram of the working process of this utility model.

[0021] In the diagram: 1-Receiver component, 2-Supporting foot, 3-Multi-rotor UAV, 4-Temperature control component, 5-Collection device, 6-Protective device, 7-Connecting device, 8-Positioning rod, 9-Pressing crossbar, 10-Temperature and humidity sensor, 11-Bolt, 12-Plastic round plate, 13-Supporting frame, 14-Supporting base plate, 15-Buffer spring, 16-Supporting cavity, 17-Insulated cargo box, 18-Drawer, 19-Guide rail, 20-Plastic strip, 21-U-shaped positioning frame, 22-Electric push rod, 23-Ground signal receiving device, 24-Temperature and humidity alarm module. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0023] Please see Figure 1-4 One embodiment of this utility model is a low-altitude logistics monitoring device based on a temperature and humidity sensor, comprising a multi-rotor drone 3. A receiving component 1 is fixedly installed at the bottom center of the multi-rotor drone 3. Support feet 2 are symmetrically fixedly installed at the bottom of the multi-rotor drone 3, and the support feet 2 are located on both sides of the receiving component 1. The receiving component 1 includes a temperature control component 4 and a collection device 5. The temperature control component 4 is fixedly installed at the bottom center of the collection device 5. The temperature control component 4 includes a protective device 6 and a connecting device 7. The protective device 6 is fixedly installed inside the center of the connecting device 7.

[0024] The protective device 6 includes a positioning rod 8, a pressing crossbar 9, a temperature and humidity sensor 10, bolts 11, a plastic round plate 12, a support frame 13, and a support base plate 14. The positioning rod 8 is fixedly installed at the four corners of the bottom of the temperature and humidity sensor 10. The support base plate 14 is fixedly installed at the four corners inside the support frame 13. The plastic round plate 12 is fixedly installed at the four corners outside the support frame 13. The bolts 11 are symmetrically rotated and installed at the top of the support frame 13. The pressing crossbar 9 is threaded onto the outer ring of the bolts 11. A plastic sheet is fixedly installed on the outer ring of the plastic round plate 12 to prevent rigid collision between the plastic round plate 12 and the support cavity 16.

[0025] The connecting device 7 includes a buffer spring 15 and a support cavity 16. The buffer spring 15 is symmetrically fixedly installed at the top inside the support cavity 16. The connecting device 7 includes a buffer spring 15, a support cavity 16, a plastic strip 20, a U-shaped positioning bracket 21, and an electric push rod 22. The buffer spring 15 is symmetrically fixedly installed at the top inside the support cavity 16, the electric push rod 22 is symmetrically fixedly installed at the bottom inside the support cavity 16, the U-shaped positioning bracket 21 is fixedly installed on the end of the electric push rod 22 near the buffer spring 15, and the plastic strip 20 is fixedly installed on the U-shaped positioning bracket 21. The positioning frame 21 is located on the side opposite to the electric push rod 22. The collection device 5 includes an insulated cargo box 17, a drawer 18, and a guide rail 19. The guide rail 19 is symmetrically fixed on both sides of the interior of the insulated cargo box 17. The drawer 18 is slidably inserted into the guide rail 19. The collection device 5 includes an insulated cargo box 17, a drawer 18, and a guide rail 19. The guide rail 19 is symmetrically fixed on both sides of the interior of the insulated cargo box 17. The drawer 18 is slidably inserted into the guide rail 19. By setting the buffer spring 15, the vibration of the insulated cargo box 17 transmitted to the temperature and humidity sensor 10 can be reduced.

[0026] The support frame 13 is fixedly installed on the end of the buffer spring 15 away from the support cavity 16. The support cavity 16 is fixedly installed at the bottom center of the insulated cargo box 17. The insulated cargo box 17 is fixedly installed at the bottom center of the multi-rotor UAV 3 and can support the placement of goods.

[0027] The positioning rod 8 is slidably inserted into the top of the support base plate 14. By sliding the positioning rod 8 into the top of the support base plate 14, the temperature and humidity sensor 10 can be placed.

[0028] The drawer 18 has keyed buttons fixedly installed on both sides, and the guide rail 19 has a slot near the inside of the drawer 18. The temperature and humidity sensor 10 is wirelessly connected to the ground signal receiver 23. The multi-rotor UAV 3 is equipped with a temperature and humidity alarm module 24. The temperature and humidity sensor 10 collects the temperature and humidity inside the insulated cargo compartment 17 and transmits the data to the ground signal receiver 23, so that the signal receiver 23 can display the temperature and humidity inside the insulated cargo compartment 17 in real time. The signal receiver 23 can be a mobile phone, remote control, or computer screen. At the same time, the temperature and humidity sensor 10 collects the temperature and humidity inside the insulated cargo compartment 17 and transmits the data to the flight control system in the multi-rotor UAV 3. The flight control system is equipped with the temperature and humidity alarm module 24. At the same time, there is a wireless signal connection between the ground multi-rotor UAV remote control device and the temperature and humidity alarm module 24, so that the ground multi-rotor UAV remote control device can display the temperature and humidity inside the insulated cargo compartment 17 and alarm information in real time.

[0029] Working principle: In use, goods are placed on drawer 18, and then drawer 18 is pushed into the insulated cargo compartment 17, allowing for layered placement of goods. Simultaneously, the drawer 18 slides along the guide rail 19 via latches on both sides, supporting its linear movement. The insulated cargo compartment 17 prevents goods from spoiling or melting during transport. After the goods are placed, the cabinet door of the insulated cargo compartment 17 can be closed to prevent goods from falling during transport. Then, the multi-rotor drone 3 can be activated and ascend to a designated altitude to transport the goods. During transport, sensors within the insulated cargo compartment 17 communicate with the interior of the compartment. This allows the temperature and humidity sensor 10 to record and sense the temperature inside the insulated cargo compartment 17 in real time. Simultaneously, the temperature and humidity sensor 10 has a wireless signal connection to an external display terminal, enabling it to send signals to the display terminal for users to monitor the temperature inside the insulated cargo compartment 17. When the support legs 2 need to land, the multi-rotor drone 3 can make contact with the ground. The buffer spring 15 absorbs the vibration potential energy of the multi-rotor drone 3, preventing it from being transmitted to the temperature and humidity sensor 10. Furthermore, the plastic circular plate 12 prevents the temperature and humidity sensor 10 from colliding with the inner wall of the support cavity 16 during shaking, thus preventing damage to the sensor 10 from vibrations and completing the cargo transportation process. In operation, when the temperature and humidity sensor 10 needs to be installed, it can be placed inside the support frame 13 until the positioning rod 8 is inserted into the support base plate 14. Simultaneously, the pressing crossbar 9 can be rotated until it is perpendicularly aligned with the edge of the temperature and humidity sensor 10. Then, the bolt 11 is tightened to move the pressing crossbar 9 downwards, thus pressing and confining the temperature and humidity sensor 10 onto the support base plate 14. During use, the combination of the buffer spring 15 and the plastic circular plate 12 prevents vibrations from the multi-rotor drone 3 during landing from affecting the temperature and humidity sensor 10, extending its service life. Furthermore, the sensing head in the temperature and humidity sensor 10... The insulated cargo compartment 17 is internally interconnected, allowing the temperature inside the compartment to be transmitted in real time to the temperature and humidity sensor 10 for display. When the multi-rotor drone 3 is in flight mode, the electric push rod 22 can be activated, causing the U-shaped positioning frame 21 to move towards the center of the support cavity 16 until it contacts the outer surface of the support frame 13. This fixes and secures the support frame 13, preventing the temperature and humidity sensor 10 from shaking during flight. Simultaneously, the plastic strip 20 prevents the U-shaped positioning frame 21 from damaging the surface of the support frame 13, thus completing the positioning of the support frame 13. When the multi-rotor drone 3 needs to land, the electric push rod 22 can be activated again.The U-shaped positioning frame 21 is moved away from the support frame 13, allowing it to disengage. At this point, a gap exists between the support frame 13 and the support cavity 16, and the buffer spring 15 is connected to the outer surface of the support frame 13. This allows the support frame 13 to sway up and down inside the support cavity 16 during landing, preventing the temperature and humidity sensor 10 from colliding with the support cavity 16. In use, the multi-rotor drone 3 has a built-in wireless communication module that is wirelessly connected to the temperature and humidity sensor 10 and the temperature and humidity alarm module 24, enabling the wireless communication module to transmit information about the temperature and humidity sensor 10's operation to the outside world.

[0030] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A low-altitude logistics monitoring device based on temperature and humidity sensors, comprising a multi-rotor drone (3), wherein a receiving component (1) is fixedly installed at the center of the bottom end of the multi-rotor drone (3), and support feet (2) are symmetrically fixedly installed at the bottom end of the multi-rotor drone (3), and the support feet (2) are located on both sides of the receiving component (1), characterized in that: The receiving component (1) includes a temperature control component (4) and a collecting device (5). The temperature control component (4) is fixedly installed at the bottom center of the collecting device (5). The temperature control component (4) includes a protective device (6) and a connecting device (7). The protective device (6) is fixedly installed at the internal center of the connecting device (7).

2. The low-altitude logistics monitoring device based on a temperature and humidity sensor according to claim 1, characterized in that: The protective device (6) includes a positioning rod (8), a pressing crossbar (9), a temperature and humidity sensor (10), a bolt (11), a plastic round plate (12), a support frame (13), and a support base plate (14). The positioning rod (8) is fixedly installed at the four corners of the bottom of the temperature and humidity sensor (10). The support base plate (14) is fixedly installed at the four corners inside the support frame (13). The plastic round plate (12) is fixedly installed at the four corners outside the support frame (13). The bolt (11) is symmetrically rotated and installed at the top of the support frame (13). The pressing crossbar (9) is threaded onto the outer ring of the bolt (11).

3. The low-altitude logistics monitoring device based on a temperature and humidity sensor according to claim 2, characterized in that: The connecting device (7) includes a buffer spring (15), a support cavity (16), a plastic strip (20), a U-shaped positioning frame (21), and an electric push rod (22). The buffer spring (15) is symmetrically fixedly installed at the top of the inside of the support cavity (16). The electric push rod (22) is symmetrically fixedly installed at the bottom of the inside of the support cavity (16). The U-shaped positioning frame (21) is fixedly installed on the end of the electric push rod (22) near the buffer spring (15). The plastic strip (20) is fixedly installed on the side of the U-shaped positioning frame (21) away from the electric push rod (22). The collecting device (5) includes an insulated cargo compartment (17), a drawer (18), and a guide rail (19). The guide rail (19) is symmetrically fixedly installed on both sides of the inside of the insulated cargo compartment (17). The drawer (18) is slidably inserted into the guide rail (19).

4. A low-altitude logistics monitoring device based on a temperature and humidity sensor according to claim 3, characterized in that: The support frame (13) is fixedly installed on the end of the buffer spring (15) away from the support cavity (16), the support cavity (16) is fixedly installed at the bottom center of the insulated cargo box (17), and the insulated cargo box (17) is fixedly installed at the bottom center of the multi-rotor UAV (3).

5. A low-altitude logistics monitoring device based on a temperature and humidity sensor according to claim 4, characterized in that: The positioning rod (8) is slidably inserted into the top of the support base plate (14).

6. A low-altitude logistics monitoring device based on a temperature and humidity sensor according to claim 5, characterized in that: The drawer (18) is fixedly equipped with keypads on both sides, and the guide rail (19) is provided with slots near the inside of the drawer (18). The temperature and humidity sensor (10) is wirelessly connected to the ground signal receiving device (23). The multi-rotor UAV (3) is equipped with a temperature and humidity alarm module (24).

Citation Information

Patent Citations

  • Logistics unmanned aerial vehicle and logistics transportation system

    CN209553514U